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NASA's program on icing research and technologyNASA's program in aircraft icing research and technology is reviewed. The program relies heavily on computer codes and modern applied physics technology in seeking icing solutions on a finer scale than those offered in earlier programs. Three major goals of this program are to offer new approaches to ice protection, to improve our ability to model the response of an aircraft to an icing encounter, and to provide improved techniques and facilities for ground and flight testing. This paper reviews the following program elements: (1) new approaches to ice protection; (2) numerical codes for deicer analysis; (3) measurement and prediction of ice accretion and its effect on aircraft and aircraft components; (4) special wind tunnel test techniques for rotorcraft icing; (5) improvements of icing wind tunnels and research aircraft; (6) ground de-icing fluids used in winter operation; (7) fundamental studies in icing; and (8) droplet sizing instruments for icing clouds.
Document ID
19890013198
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reinmann, John J.
(NASA Lewis Research Center Cleveland, OH, United States)
Shaw, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Ranaudo, Richard J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:101989
E-4692
NASA-TM-101989
Report Number: NAS 1.15:101989
Report Number: E-4692
Report Number: NASA-TM-101989
Meeting Information
Meeting: Symposium on Flight in Adverse Environmental Conditions
Location: Gol
Country: Norway
Start Date: May 8, 1989
End Date: May 12, 1989
Sponsors: AGARD
Accession Number
89N22569
Funding Number(s)
PROJECT: RTOP 505-68-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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